Incident · minor damage
Dec 17, 1990 · NEVIS- Damage
- Minor
- Report
- MIA91WA046
From NTSB records; matched by N-number.Read NTSB report (search CAROL for MIA91WA046)
N676MF1971 Cessna 402B
Registration validUnclaimedSource: FAA, updated Oct 17, 2026
Safety record in brief:1 NTSB incident (minor damage, Dec 1990)9 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Coastal Resource Associates INC
- Owner type
- Corporation
- City, state
- Christiansted, VI
- Certificate issued
- May 24, 1988
- Expires
- Jun 30, 2027
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jul 31, 1971
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 402B
- Year
- 1971
- Serial number
- 402B0106
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A8F31B
Engine
- Make and model
- Cont Motor Gtsio-520-C
- Type
- Reciprocating
- Power
- 340 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1988 – nowCoastal Resource Associates INCChristiansted, VI · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (1)
ADs published since 1998 that may apply (9)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (GTSIO-520-C) |
| 2020-16-11 | Reciprocating Cylinder Section | Sep 21, 2020 | Engine (GTSIO-520-C)Only with: Engines originally manufactured, rebuilt, or modified with a cross-flow cylinder assembly replacement on or after November 1, 2014, with cross-flow cylinder assembly P/N 658538, 658540, 658542, 658591, 658595, 658613, 658624, 658539, 658541, 658590, 658594, 658603, 658623, or 658630 installed. |
| 2016-17-08 | Elevator Tab Control System | Sep 12, 2016 | Airframe (402B) |
| 2009-04-04 | Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, and 402B Airplanes | Mar 2, 2009 | Airframe (402B)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; … |
| 2007-05-15 | Teledyne Continental Motors GTSIO-520 Series Reciprocating Engines | Apr 16, 2007 | Engine (GTSIO-520-C) |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (402B)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50. |
| 2005-12-12 | Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 411, and 411A Airplanes | Jun 22, 2005 | Airframe (402B) |
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (402B) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (402B) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Stabilizers · spar · corrodedDec 12, 2000
UPON ANNUAL INSPECTION, FLAKING WAS NOTICED ON CENTER FORWARD SPAR AREA. FURTHER INSPECTION REVEALED THE SPAR WAS CORRODED 25 PERCENT THROUGH MAIN SURFACE. UNIT WAS REPLACED WITH AN AIRWORTHY ITEM.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · spar · corrodedDec 12, 2000
UPON ANNUAL INSPECTION, FLAKING WAS NOTICED ON AFT SPAR AREA. FURTHER INSPECTION REVEALED THE SPAR WAS CORRODED .2500 THROUGH MAIN SURFACE. UNIT WAS REPLACED WITH AN AIRWORTHY ITEM.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026